Pages that link to "Item:Q362974"
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The following pages link to Error analysis and a new steering law design for spacecraft control system using SGCMGs (Q362974):
Displaying 10 items.
- Influence of flexible solar arrays on vibration isolation platform of control moment gyroscopes (Q315357) (← links)
- An improved constrained steering law for SGCMGs with DPC (Q358788) (← links)
- Attitude control of a rigid spacecraft with one variable-speed control moment gyro (Q740030) (← links)
- Steering laws analysis of sgcmgs based on singular value decomposition theory (Q940702) (← links)
- Singularity penetration with unit delay (SPUD) (Q1657275) (← links)
- Path planning for rapid large-angle maneuver of satellites based on the Gauss pseudospectral method (Q1792646) (← links)
- Calculation of controls, not generating singularities for four control moment gyrodynes (Q1995362) (← links)
- Singularity avoidance controller design for spacecraft attitude control using double-gimbal variable-speed control moment gyro (Q2687848) (← links)
- Spacecraft attitude control by combination of various torquers (Q3644975) (← links)
- Approach to control moment gyroscope steering using feedback linearization (Q3984655) (← links)